What was found
LOWER FUSELAGE ACCESS PANEL 193D SEVERAL FASTENER HOLE ELONGATED / [01] PERFORMED VISUAL INSPECTION AT PANEL #193D FOUND ALL FASTENER HOLE DAMAGE AS PER BOEING 737 NTM 51-05-01 AND PREPARED PANEL FOR DRY-OUT PER BOEING 737 SRM 51-70-05-2R-0;[02] VERIFIED STEP 1. OK TO DRY OUT.;[03] ACCOMPLISHED DRY OUT AT PANEL 193D AS PER B737 SRM 51-70-05-2R-0;[04] VERIFIED DRY OUT.<BR>OK TO REPAIR;[05] REPAIRED ALL DAMAGE HOLES AT LOWER FUSELAGE PANEL #193D AS PER B737 SRM 51-70-05-2R-8. MATERIAL USED BMS8-79 PO#1759636 PLUS BMS5-129-TY2CL2EGR5 PO#1759850.;[06] VERIFIED STEP 5;[07] TOUCHED UP PAINT ON LOWER FUSELAGE ACCESS PANEL 193D REF B-737 AMM 51-21-72-370-804 AND 51-21-73-370-803;[08] VERIFIED STEP 7. TASK C/W